View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 28932U 26134.30142470 +.00000000 +00000-0 +22770-3 0 00005
2 28932 98.2522 287.0859 0051260 19.5229 340.7950 15.17641713 09
| Epoch (UTC): | 14 May 2026 07:14:03 |
| Eccentricity: | 0.0051260 |
| inclination: | 98.2522° |
| perigee height: | 478 km |
| apogee height: | 548 km |
| right ascension of ascending node: | 287.0859° |
| argument of perigee: | 19.5229° |
| revolutions per day: | 15.17641713 |
| mean anomaly at epoch: | 340.7950° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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